Flugzeug mit Symmetrischen Antriebssystem-Drehmustern
Anmelder: RTX Corporation 🇺🇸
Details
- Veröffentlichungs-Nr.
- EP4756200
- Anmeldetag
- 5. Dezember 2025
- Veröffentlichung
- 10. Juni 2026
- Rechtsraum
- EP
Abstract
A first core turbine rotor of a first propulsion system (24A) is disposed in a first core turbine section (89) and is configured to rotate in a first rotational direction. A first power turbine rotor (106) is disposed in a first power turbine section (90) and is configured to rotate in the first rotational direction. The first power turbine rotor is operatively coupled to a first open propulsor rotor (58). A second core turbine rotor of a second propulsion system (24B) is disposed in a second core turbine section and is configured to rotate in the first rotational direction. A second power turbine rotor is disposed in a second power turbine section and is configured to rotate in a second rotational direction that is opposite the first rotational direction. The second power turbine rotor is operatively coupled to a second open propulsor rotor (58).
Anmelder
- Firma
- RTX Corporation
- Land
- 🇺🇸 USA
US-amerikanischer Luft- und Raumfahrt- sowie Verteidigungskonzern, entstanden aus Raytheon und United Technologies. Entwickelt und fertigt Triebwerke, Avionik, Radarsysteme, Raketen- und Verteidigungstechnik für zivile und militärische Kunden.
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